US2017194714A1PendingUtilityA1
Cooled antenna feed for a telescope array
Est. expiryJan 6, 2036(~9.4 yrs left)· nominal 20-yr term from priority
H01Q 19/132H01Q 1/005H01Q 15/16H01Q 21/0025H01Q 19/19
34
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Claims
Abstract
An offset Gregorian antenna used in radio astronomy. The antenna may include a primary reflector having a substantially paraboloidal shape and a secondary reflector having substantially an ellipsoidal shape. The secondary reflector may be displaced from the optical axis of the primary reflector. The antenna may also include a feed located substantially coincident with the second focus of the secondary reflector. The feed may be located within a vacuum sealed enclosure, and a cryo pump may be used to cool the feed within the enclosure. Also, a shroud may partially surrounding the feed.
Claims
exact text as granted — not AI-modifiedWhat is claimed:
1 . An offset Gregorian antenna, comprising:
a primary reflector having a substantially paraboloidal shape; a secondary reflector having substantially an ellipsoidal shape, displaced from the optical axis of the primary reflector; a feed located substantially coincident with the second focus of the secondary reflector; a cryo pump to cool the feed; and a shroud partially surrounding the feed.
2 . The antenna of claim 1 , wherein the first focus of said secondary reflector is substantially coincident with the focus of the primary reflector
3 . The antenna of claim 1 , wherein the shroud is located between the feed and a ground while providing substantially unimpeded passage of radiation between the feed and the primary reflector and the secondary reflector.
4 . The antenna of claim 1 , wherein the primary reflector has a diameter of about 6 meters.
5 . The antenna of claim 1 , wherein the secondary reflector has a diameter of about 2 meters.
6 . The antenna of claim 1 , further comprising an enclosure surrounding the feed.
7 . The antenna of claim 6 , wherein the enclosure is vacuumed sealed.
8 . The antenna of claim 6 , further comprising a polyethylene anti-reflective material covers a portion of the enclosure.
9 . The antenna of claim 6 , wherein the enclosure is made of borosilicate glass.
10 . The antenna of claim 6 , wherein the enclosure is made of fused quartz.
11 . The antenna of claim 6 , wherein the enclosure is made of composite materials.
12 . The antenna of claim 1 , wherein the feed includes a low noise amplifier.
13 . The antenna of claim 12 , wherein the low noise amplifier includes a chassis, an input coax cable connected to one end of the chassis and an output coax cable connected to an opposite end of the chassis.
14 . The antenna of claim 13 , wherein the resistance of the input coax cable is about 95 ohm.
15 . The antenna of claim 13 , wherein the resistance of the output coax cable is about 50 ohm.
16 . The antenna of claim 12 , wherein the low noise amplifier is disposed at a tip of the feed.
17 . The antenna of claim 1 , wherein the feed includes a thin rexolite standoff
18 . The antenna of claim 1 , further comprising a vibration isolation mechanism connected to the feed to dampen vibrations.
19 . An offset Gregorian antenna, comprising:
a primary reflector having a substantially paraboloidal shape; a secondary reflector having substantially an ellipsoidal shape, displaced from the optical axis of the primary reflector; a feed located substantially coincident with the second focus of the secondary reflector; a vacuum sealed enclosure surrounding the feed; and a cryo pump in communication with the vacuum sealed enclosure to cool the feed within the vacuum sealed enclosure.
20 . The antenna of claim 19 , wherein the cryo pump cools the feed within the vacuum sealed enclosure to less than 65 K.Join the waitlist — get patent alerts
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